Date: June 19th 2010

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 11840 3 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP


There are no maneuvers



Coasting Arc #1 (Orbit 2359)
---------------------------------------

Vector Time (GMT): 2010/168/23:49:42
916
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4520243
48                 A    =         6727683
45  meter
 Y    =         973253
28  meter          E    =           
0009781
 Z    =       -4892135
65                 I    =           51
38931
 XDOT =      -3751
265792                 Wp   =           56
83140
 YDOT =      -6341
261124  meter/sec      RA   =          225
51407  deg
 ZDOT =       2213
011875                 TA   =          234
72398
                                          MA   =          234
81552
                                          Ha   =            194
595  n
mi
                                          Hp   =            187
237

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14830195
13                 X    =        -4507025
64
 Y    =        3193088
19  feet           Y    =          922779
71  meter
 Z    =      -16050313
80                 Z    =        -4914062
65
 XDOT =     -12307
302466                 XDOT =       -3690
828208
 YDOT =     -20804
662481  feet/sec       YDOT =       -6382
872351  meter/sec
 ZDOT =       7260
537646                 ZDOT =        2194
934380

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1313631
25                 X    =         -400394
80
 Y    =      -15019691
27  feet           Y    =        -4578001
90  meter
 Z    =      -16137729
70                 Z    =        -4918780
01
 XDOT =      21097
460322                 XDOT =        6430
505906
 YDOT =      -9539
023175  feet/sec       YDOT =       -2907
494264  meter/sec
 ZDOT =       7188
386138                 ZDOT =        2191
020095


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10169
00499183  
00016717  00000-0  10270-3 0  9008
2 25544  51
6475 226
4313 0009681 336
3150  23
7565 15
71894561 23602


Satellite: ISS
Catalog Number: 25544
Epoch time:      10169
00499183   =   yrday
fracday
Element set:     900
Inclination:       51
6475  deg
RA of node:       226
4313  deg
Eccentricity:     
0009681     
Arg of perigee:   336
3150  deg
Mean anomaly:      23
7565  deg
Mean motion:   15
71894561  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2360
Checksum:              304


Coasting Arc #2 (Orbit 2375)
---------------------------------------

Vector Time (GMT): 2010/169/23:49:42
916
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4297595
94                 A    =         6737536
97  meter
 Y    =        5024312
80  meter          E    =           
0002794
 Z    =       -1304627
25                 I    =           51
44417
 XDOT =      -4459
003993                 Wp   =           49
66463
 YDOT =       2302
782071  meter/sec      RA   =          220
40899  deg
 ZDOT =      -5826
550674                 TA   =          144
66849
                                          MA   =          144
64997
                                          Ha   =            194
820  n
mi
                                          Hp   =            187
226

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14099724
22                 X    =         4247431
39
 Y    =       16483965
89  feet           Y    =         5072090
74  meter
 Z    =       -4280273
14                 Z    =        -1283870
85
 XDOT =     -14629
278191                 XDOT =       -4456
118421
 YDOT =       7555
059288  feet/sec       YDOT =        2252
935613  meter/sec
 ZDOT =     -19115
979903                 ZDOT =       -5848
205227

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17921640
59                 X    =        -5462516
05
 Y    =       12249095
41  feet           Y    =         3733524
28  meter
 Z    =       -4197446
00                 Z    =        -1279381
54
 XDOT =      -5038
409628                 XDOT =       -1535
707255
 YDOT =     -13944
458977  feet/sec       YDOT =       -4250
271096  meter/sec
 ZDOT =     -19202
297960                 ZDOT =       -5852
860418


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10170
02219117  
00016717  00000-0  10270-3 0  9010
2 25544  51
6476 221
2246 0009586 339
6130  20
4648 15
71867183 23762


Satellite: ISS
Catalog Number: 25544
Epoch time:      10170
02219117   =   yrday
fracday
Element set:     901
Inclination:       51
6476  deg
RA of node:       221
2246  deg
Eccentricity:     
0009586     
Arg of perigee:   339
6130  deg
Mean anomaly:      20
4648  deg
Mean motion:   15
71867183  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2376
Checksum:              296


Coasting Arc #3 (Orbit 2391)
---------------------------------------

Vector Time (GMT): 2010/170/23:49:42
916
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3083478
39                 A    =         6726160
50  meter
 Y    =       -2916811
93  meter          E    =           
0010765
 Z    =        5218932
36                 I    =           51
43036
 XDOT =       5897
058136                 Wp   =             
19294
 YDOT =       4891
135905  meter/sec      RA   =          215
25613  deg
 ZDOT =       -739
919499                 TA   =           96
93072
                                          MA   =           96
80826
                                          Ha   =            194
840  n
mi
                                          Hp   =            186
838

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10116398
91                 X    =         3090512
83
 Y    =       -9569592
95  feet           Y    =        -2882291
92  meter
 Z    =       17122481
49                 Z    =         5233928
69
 XDOT =      19347
303596                 XDOT =        5845
520690
 YDOT =      16047
033810  feet/sec       YDOT =        4956
792252  meter/sec
 ZDOT =      -2427
557410                 ZDOT =        -711
396098

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8611490
08                 X    =         2624782
18
 Y    =       10849454
93  feet           Y    =         3306913
86  meter
 Z    =       17182245
92                 Z    =         5237148
56
 XDOT =     -16961
736064                 XDOT =       -5169
937152
 YDOT =      17182
147055  feet/sec       YDOT =        5237
118422  meter/sec
 ZDOT =      -2313
751978                 ZDOT =        -705
231603


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10171
03937748  
00016717  00000-0  10270-3 0  9020
2 25544  51
6476 216
0171 0009745 343
8703  16
2148 15
71932820 23928


Satellite: ISS
Catalog Number: 25544
Epoch time:      10171
03937748   =   yrday
fracday
Element set:     902
Inclination:       51
6476  deg
RA of node:       216
0171  deg
Eccentricity:     
0009745     
Arg of perigee:   343
8703  deg
Mean anomaly:      16
2148  deg
Mean motion:   15
71932820  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2392
Checksum:              302


Coasting Arc #4 (Orbit 2406)
---------------------------------------

Vector Time (GMT): 2010/171/23:49:42
916
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5828411
75                 A    =         6738041
08  meter
 Y    =       -3356446
60  meter          E    =           
0019271
 Z    =         -28434
49                 I    =           51
49501
 XDOT =       2376
326353                 Wp   =           19
74170
 YDOT =      -4167
347809  meter/sec      RA   =          210
12935  deg
 ZDOT =       6029
731715                 TA   =          339
94877
                                          MA   =          340
02438
                                          Ha   =            195
017  n
mi
                                          Hp   =            186
623

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19122085
80                 X    =        -5790308
04
 Y    =      -11011963
91  feet           Y    =        -3421410
32  meter
 Z    =         -93289
00                 Z    =          -56657
00
 XDOT =       7796
346304                 XDOT =        2393
458244
 YDOT =     -13672
400948  feet/sec       YDOT =       -4140
679345  meter/sec
 ZDOT =      19782
584368                 ZDOT =        6041
317030

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12405015
79                 X    =         3781048
81
 Y    =      -18248271
49  feet           Y    =        -5562073
15  meter
 Z    =        -205883
94                 Z    =          -62753
42
 XDOT =      11731
387422                 XDOT =        3575
726886
 YDOT =       7771
341127  feet/sec       YDOT =        2368
704775  meter/sec
 ZDOT =      19828
734848                 ZDOT =        6043
798382


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10171
99298090  
00016717  00000-0  10270-3 0  9036
2 25544  51
6469 211
1352 0009814 347
3474  12
7441 15
71942899 24079


Satellite: ISS
Catalog Number: 25544
Epoch time:      10171
99298090   =   yrday
fracday
Element set:     903
Inclination:       51
6469  deg
RA of node:       211
1352  deg
Eccentricity:     
0009814     
Arg of perigee:   347
3474  deg
Mean anomaly:      12
7441  deg
Mean motion:   15
71942899  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2407
Checksum:              319


Coasting Arc #5 (Orbit 2422)
---------------------------------------

Vector Time (GMT): 2010/172/23:49:42
916
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -959470
25                 A    =         6726141
45  meter
 Y    =        4141563
76  meter          E    =           
0017319
 Z    =       -5224849
89                 I    =           51
48053
 XDOT =      -7170
271832                 Wp   =           49
33338
 YDOT =      -2658
384004  meter/sec      RA   =          205
00579  deg
 ZDOT =       -781
093586                 TA   =          213
15001
                                          MA   =          213
25865
                                          Ha   =            195
166  n
mi
                                          Hp   =            186
310

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3147868
29                 X    =         -980329
10
 Y    =       13587807
62  feet           Y    =         4130718
60  meter
 Z    =      -17141895
95                 Z    =        -5229561
03
 XDOT =     -23524
513886                 XDOT =       -7136
217947
 YDOT =      -8721
732295  feet/sec       YDOT =       -2738
375727  meter/sec
 ZDOT =      -2562
642999                 ZDOT =        -815
844744

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13390405
16                 X    =        -4081395
49
 Y    =       -3819924
05  feet           Y    =        -1164312
85  meter
 Z    =      -17160635
70                 Z    =        -5230561
76
 XDOT =       9775
706177                 XDOT =        2979
635243
 YDOT =     -21994
265177  feet/sec       YDOT =       -6703
852026  meter/sec
 ZDOT =      -2701
278380                 ZDOT =        -823
349650


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10173
01014641  
00016717  00000-0  10270-3 0  9040
2 25544  51
6456 205
9275 0009859 351
1382   8
9604 15
71963672 24238


Satellite: ISS
Catalog Number: 25544
Epoch time:      10173
01014641   =   yrday
fracday
Element set:     904
Inclination:       51
6456  deg
RA of node:       205
9275  deg
Eccentricity:     
0009859     
Arg of perigee:   351
1382  deg
Mean anomaly:       8
9604  deg
Mean motion:   15
71963672  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2423
Checksum:              302


Coasting Arc #6 (Orbit 2438)
---------------------------------------

Vector Time (GMT): 2010/173/23:49:42
916
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6491258
66                 A    =         6737122
52  meter
 Y    =        1235406
08  meter          E    =           
0011589
 Z    =        1313491
87                 I    =           51
54591
 XDOT =        235
973057                 Wp   =           76
00312
 YDOT =       5009
560650  meter/sec      RA   =          199
85809  deg
 ZDOT =      -5832
203793                 TA   =           89
58068
                                          MA   =           89
44788
                                          Ha   =            195
283  n
mi
                                          Hp   =            186
067

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21296780
39                 X    =         6470580
93
 Y    =        4053169
55  feet           Y    =         1307879
35  meter
 Z    =        4309356
54                 Z    =         1344976
61
 XDOT =        774
189820                 XDOT =         208
269670
 YDOT =      16435
566438  feet/sec       YDOT =        5012
045605  meter/sec
 ZDOT =     -19134
526881                 ZDOT =       -5831
123809

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4903139
18                 X    =        -1494476
82
 Y    =       21091276
40  feet           Y    =         6428621
05  meter
 Z    =        4434960
88                 Z    =         1351776
08
 XDOT =     -14919
296323                 XDOT =       -4547
401519
 YDOT =        584
910791  feet/sec       YDOT =         178
280809  meter/sec
 ZDOT =     -19130
160195                 ZDOT =       -5830
872828


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10174
02730088  
00016717  00000-0  10270-3 0  9053
2 25544  51
6457 200
7208 0009916 355
0922   5
0141 15
71985093 24397


Satellite: ISS
Catalog Number: 25544
Epoch time:      10174
02730088   =   yrday
fracday
Element set:     905
Inclination:       51
6457  deg
RA of node:       200
7208  deg
Eccentricity:     
0009916     
Arg of perigee:   355
0922  deg
Mean anomaly:       5
0141  deg
Mean motion:   15
71985093  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2439
Checksum:              294


Coasting Arc #7 (Orbit 2454)
---------------------------------------

Vector Time (GMT): 2010/174/23:49:42
916
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1395754
96                 A    =         6727632
51  meter
 Y    =       -4389713
91  meter          E    =           
0008341
 Z    =        4896596
31                 I    =           51
54086
 XDOT =       7376
105024                 Wp   =           40
47763
 YDOT =        122
715007  meter/sec      RA   =          194
76075  deg
 ZDOT =       2216
676594                 TA   =           27
98343
                                          MA   =           27
93861
                                          Ha   =            195
478  n
mi
                                          Hp   =            185
971

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4579248
57                 X    =        -1370351
50
 Y    =      -14401948
52  feet           Y    =        -4405181
00  meter
 Z    =       16064948
52                 Z    =         4889876
54
 XDOT =      24199
819632                 XDOT =        7363
416345
 YDOT =        402
608291  feet/sec       YDOT =         205
127623  meter/sec
 ZDOT =       7272
561005                 ZDOT =        2252
479037

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14504730
17                 X    =         4421041
76
 Y    =       -4342885
92  feet           Y    =        -1323711
63  meter
 Z    =       16038090
72                 Z    =         4888410
05
 XDOT =      -1272
913373                 XDOT =        -387
983996
 YDOT =      23083
157233  feet/sec       YDOT =        7035
746325  meter/sec
 ZDOT =       7415
394412                 ZDOT =        2260
212217


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10175
04444536  
00016717  00000-0  10270-3 0  9067
2 25544  51
6443 195
5123 0009897 359
1884    
9260 15
71946901 24558


Satellite: ISS
Catalog Number: 25544
Epoch time:      10175
04444536   =   yrday
fracday
Element set:     906
Inclination:       51
6443  deg
RA of node:       195
5123  deg
Eccentricity:     
0009897     
Arg of perigee:   359
1884  deg
Mean anomaly:        
9260  deg
Mean motion:   15
71946901  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2455
Checksum:              319


Coasting Arc #8 (Orbit 2469)
---------------------------------------

Vector Time (GMT): 2010/175/23:49:42
916
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6152475
84                 A    =         6734996
19  meter
 Y    =         998233
98  meter          E    =           
0013667
 Z    =       -2535260
06                 I    =           51
59475
 XDOT =      -2944
212217                 Wp   =           19
14810
 YDOT =      -4753
879179  meter/sec      RA   =          189
59519  deg
 ZDOT =       5293
812493                 TA   =          312
11390
                                          MA   =          312
22999
                                          Ha   =            195
351  n
mi
                                          Hp   =            185
710

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20185288
18                 X    =        -6150865
18
 Y    =        3275045
85  feet           Y    =          929442
85  meter
 Z    =       -8317782
35                 Z    =        -2565144
64
 XDOT =      -9659
488901                 XDOT =       -2916
551008
 YDOT =     -15596
716468  feet/sec       YDOT =       -4786
649546  meter/sec
 ZDOT =      17368
151224                 ZDOT =        5279
575730

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3159696
27                 X    =         -963075
42
 Y    =      -20154166
80  feet           Y    =        -6142990
04  meter
 Z    =       -8437011
76                 Z    =        -2571601
18
 XDOT =      14181
981376                 XDOT =        4322
667923
 YDOT =      -9442
287755  feet/sec       YDOT =       -2878
009308  meter/sec
 ZDOT =      17311
293279                 ZDOT =        5276
482192


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10175
99800495  
00016717  00000-0  10270-3 0  9072
2 25544  51
6432 190
6295 0009774   2
1123 358
0078 15
72000756 24708


Satellite: ISS
Catalog Number: 25544
Epoch time:      10175
99800495   =   yrday
fracday
Element set:     907
Inclination:       51
6432  deg
RA of node:       190
6295  deg
Eccentricity:     
0009774     
Arg of perigee:     2
1123  deg
Mean anomaly:     358
0078  deg
Mean motion:   15
72000756  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2470
Checksum:              304


Coasting Arc #9 (Orbit 2485)
---------------------------------------

Vector Time (GMT): 2010/176/23:49:42
916
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3641222
52                 A    =         6729896
55  meter
 Y    =        3702723
69  meter          E    =           
0015663
 Z    =       -4296227
66                 I    =           51
60667
 XDOT =      -6451
220678                 Wp   =           36
04758
 YDOT =       2273
799560  meter/sec      RA   =          184
51883  deg
 ZDOT =      -3502
019229                 TA   =          198
37145
                                          MA   =          198
42809
                                          Ha   =            195
549  n
mi
                                          Hp   =            185
542

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11946268
10                 X    =         3620417
54
 Y    =       12148043
60  feet           Y    =         3743326
57  meter
 Z    =      -14095235
09                 Z    =        -4278588
46
 XDOT =     -21165
422173                 XDOT =       -6459
155170
 YDOT =       7459
972309  feet/sec       YDOT =        2201
614524  meter/sec
 ZDOT =     -11489
564398                 ZDOT =       -3533
377894

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12008558
55                 X    =        -3660208
65
 Y    =       12168129
51  feet           Y    =         3708845
87  meter
 Z    =      -14024802
42                 Z    =        -4274759
78
 XDOT =      -6814
183267                 XDOT =       -2076
963060
 YDOT =     -20134
379660  feet/sec       YDOT =       -6136
958920  meter/sec
 ZDOT =     -11614
680059                 ZDOT =       -3540
154482


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10177
01512568  
00016717  00000-0  10270-3 0  9089
2 25544  51
6423 185
4219 0009811   6
7477 353
3816 15
72026968 24868


Satellite: ISS
Catalog Number: 25544
Epoch time:      10177
01512568   =   yrday
fracday
Element set:     908
Inclination:       51
6423  deg
RA of node:       185
4219  deg
Eccentricity:     
0009811     
Arg of perigee:     6
7477  deg
Mean anomaly:     353
3816  deg
Mean motion:   15
72026968  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2486
Checksum:              321


Coasting Arc #10 (Orbit 2501)
---------------------------------------

Vector Time (GMT): 2010/177/23:49:42
916
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4949938
89                 A    =         6732181
63  meter
 Y    =       -2865090
49  meter          E    =           
0017145
 Z    =        3549168
62                 I    =           51
64553
 XDOT =       5224
345004                 Wp   =           53
20176
 YDOT =       3469
979295  meter/sec      RA   =          179
34649  deg
 ZDOT =      -4460
196060                 TA   =           84
54620
                                          MA   =           84
35065
                                          Ha   =            195
521  n
mi
                                          Hp   =            185
278

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16239957
00                 X    =         4964367
92
 Y    =       -9399903
17  feet           Y    =        -2809657
35  meter
 Z    =       11644254
01                 Z    =         3573249
68
 XDOT =      17140
239516                 XDOT =        5206
821394
 YDOT =      11384
446507  feet/sec       YDOT =        3528
303940  meter/sec
 ZDOT =     -14633
189174                 ZDOT =       -4434
858308

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9859559
83                 X    =         3005193
84
 Y    =       15894548
18  feet           Y    =         4844658
29  meter
 Z    =       11740334
44                 Z    =         3578453
94
 XDOT =      -9726
030434                 XDOT =       -2964
494076
 YDOT =      16826
942795  feet/sec       YDOT =        5128
852164  meter/sec
 ZDOT =     -14532
021111                 ZDOT =       -4429
360035


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10178
03223340  
00016717  00000-0  10270-3 0  9090
2 25544  51
6427 180
2132 0009760   9
4186 350
7158 15
72050494 25029


Satellite: ISS
Catalog Number: 25544
Epoch time:      10178
03223340   =   yrday
fracday
Element set:     909
Inclination:       51
6427  deg
RA of node:       180
2132  deg
Eccentricity:     
0009760     
Arg of perigee:     9
4186  deg
Mean anomaly:     350
7158  deg
Mean motion:   15
72050494  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2502
Checksum:              283


Coasting Arc #11 (Orbit 2517)
---------------------------------------

Vector Time (GMT): 2010/178/23:49:42
916
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5340405
11                 A    =         6732616
36  meter
 Y    =       -2197163
86  meter          E    =           
0017441
 Z    =        3439504
23                 I    =           51
67650
 XDOT =       4644
250043                 Wp   =           58
47494
 YDOT =      -4104
427358  meter/sec      RA   =          174
27818  deg
 ZDOT =       4581
055678                 TA   =          342
23820
                                          MA   =          342
29910
                                          Ha   =            195
695  n
mi
                                          Hp   =            185
108

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17521014
14                 X    =        -5332147
39
 Y    =       -7208542
84  feet           Y    =        -2256837
91  meter
 Z    =       11284462
68                 Z    =         3413580
51
 XDOT =      15237
040825                 XDOT =        4667
547670
 YDOT =     -13465
969023  feet/sec       YDOT =       -4052
363167  meter/sec
 ZDOT =      15029
710230                 ZDOT =        4603
672995

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6393700
31                 X    =         1948799
86
 Y    =      -17899579
95  feet           Y    =        -5455791
97  meter
 Z    =       11180955
17                 Z    =         3407955
14
 XDOT =      12840
994655                 XDOT =        3913
935171
 YDOT =      14047
988454  feet/sec       YDOT =        4281
826881  meter/sec
 ZDOT =      15119
945423                 ZDOT =        4608
559365


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10179
04933063  
00016717  00000-0  10270-3 0  9104
2 25544  51
6421 175
0046 0009620  14
1426 346
0004 15
72073550 25187


Satellite: ISS
Catalog Number: 25544
Epoch time:      10179
04933063   =   yrday
fracday
Element set:     910
Inclination:       51
6421  deg
RA of node:       175
0046  deg
Eccentricity:     
0009620     
Arg of perigee:    14
1426  deg
Mean anomaly:     346
0004  deg
Mean motion:   15
72073550  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2518
Checksum:              265


Coasting Arc #12 (Orbit 2532)
---------------------------------------

Vector Time (GMT): 2010/179/23:49:42
916
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3027518
86                 A    =         6729243
77  meter
 Y    =        4112666
98  meter          E    =           
0013190
 Z    =       -4388976
76                 I    =           51
69594
 XDOT =      -6770
820813                 Wp   =           64
21064
 YDOT =      -1405
618248  meter/sec      RA   =          169
11116  deg
 ZDOT =       3366
826521                 TA   =          239
63001
                                          MA   =          239
76048
                                          Ha   =            195
702  n
mi
                                          Hp   =            184
806

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9932804
67                 X    =        -3051961
89
 Y    =       13493001
89  feet           Y    =         4078675
52  meter
 Z    =      -14399530
05                 Z    =        -4403742
92
 XDOT =     -22213
979044                 XDOT =       -6770
954910
 YDOT =      -4611
608425  feet/sec       YDOT =       -1481
334913  meter/sec
 ZDOT =      11046
018771                 ZDOT =        3333
933779

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14086609
39                 X    =        -4293598
54
 Y    =       -8977159
29  feet           Y    =        -2736238
15  meter
 Z    =      -14458430
79                 Z    =        -4406929
71
 XDOT =       2542
656376                 XDOT =         775
001664
 YDOT =     -21498
093653  feet/sec       YDOT =       -6552
618946  meter/sec
 ZDOT =      10914
684434                 ZDOT =        3326
795816


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10180
00284934  
00016717  00000-0  10270-3 0  9119
2 25544  51
6426 170
1217 0009637  18
9769 341
1750 15
72073428 25333


Satellite: ISS
Catalog Number: 25544
Epoch time:      10180
00284934   =   yrday
fracday
Element set:     911
Inclination:       51
6426  deg
RA of node:       170
1217  deg
Eccentricity:     
0009637     
Arg of perigee:    18
9769  deg
Mean anomaly:     341
1750  deg
Mean motion:   15
72073428  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2533
Checksum:              296


Coasting Arc #13 (Orbit 2548)
---------------------------------------

Vector Time (GMT): 2010/180/23:49:42
916
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6282926
24                 A    =         6735041
78  meter
 Y    =         198695
89  meter          E    =           
0009413
 Z    =       -2433233
64                 I    =           51
74560
 XDOT =      -2231
965109                 Wp   =           56
67591
 YDOT =       5035
356024  meter/sec      RA   =          164
04115  deg
 ZDOT =      -5361
861925                 TA   =          150
69144
                                          MA   =          150
63860
                                          Ha   =            195
818  n
mi
                                          Hp   =            184
670

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20613275
07                 X    =         6292057
47
 Y    =         651889
39  feet           Y    =          269006
73  meter
 Z    =       -7983050
01                 Z    =        -2402689
41
 XDOT =      -7322
720174                 XDOT =       -2262
058908
 YDOT =      16520
196928  feet/sec       YDOT =        5010
229383  meter/sec
 ZDOT =     -17591
410516                 ZDOT =       -5372
777016

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1007668
99                 X    =          307137
51
 Y    =       20645798
18  feet           Y    =         6292839
28  meter
 Z    =       -7861092
63                 Z    =        -2396061
03
 XDOT =     -15539
896370                 XDOT =       -4736
560414
 YDOT =      -5943
753139  feet/sec       YDOT =       -1811
655957  meter/sec
 ZDOT =     -17634
928336                 ZDOT =       -5375
126157


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10181
01992247  
00016717  00000-0  10270-3 0  9125
2 25544  51
6431 164
9138 0009822  22
7372 337
4223 15
72118948 25498


Satellite: ISS
Catalog Number: 25544
Epoch time:      10181
01992247   =   yrday
fracday
Element set:     912
Inclination:       51
6431  deg
RA of node:       164
9138  deg
Eccentricity:     
0009822     
Arg of perigee:    22
7372  deg
Mean anomaly:     337
4223  deg
Mean motion:   15
72118948  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2549
Checksum:              307


Coasting Arc #14 (Orbit 2564)
---------------------------------------

Vector Time (GMT): 2010/181/23:49:42
916
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         827557
77                 A    =         6727048
30  meter
 Y    =       -4490683
52  meter          E    =           
0015305
 Z    =        4935461
92                 I    =           51
74689
 XDOT =       7327
157972                 Wp   =           38
95491
 YDOT =      -1019
472238  meter/sec      RA   =          158
88941  deg
 ZDOT =      -2140
933874                 TA   =           71
86100
                                          MA   =           71
69440
                                          Ha   =            195
886  n
mi
                                          Hp   =            184
534

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2715084
54                 X    =          853736
63
 Y    =      -14733213
64  feet           Y    =        -4481283
54  meter
 Z    =       16192460
35                 Z    =         4939545
15
 XDOT =      24039
232193                 XDOT =        7348
413462
 YDOT =      -3344
725190  feet/sec       YDOT =        -937
416464  meter/sec
 ZDOT =      -7024
061265                 ZDOT =       -2105
287490

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14917693
75                 X    =         4546913
05
 Y    =        1172706
28  feet           Y    =          357440
88  meter
 Z    =       16208707
96                 Z    =         4940414
19
 XDOT =       5758
717970                 XDOT =        1755
257237
 YDOT =      22552
527525  feet/sec       YDOT =        6874
010390  meter/sec
 ZDOT =      -6881
734005                 ZDOT =       -2097
552525


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10182
03698528  
00016717  00000-0  10270-3 0  9134
2 25544  51
6428 159
7052 0009626  27
2611 332
9055 15
72076932 25656


Satellite: ISS
Catalog Number: 25544
Epoch time:      10182
03698528   =   yrday
fracday
Element set:     913
Inclination:       51
6428  deg
RA of node:       159
7052  deg
Eccentricity:     
0009626     
Arg of perigee:    27
2611  deg
Mean anomaly:     332
9055  deg
Mean motion:   15
72076932  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2565
Checksum:              314


Coasting Arc #15 (Orbit 2580)
---------------------------------------

Vector Time (GMT): 2010/182/23:49:42
916
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6298058
43                 A    =         6736812
73  meter
 Y    =        1980387
42  meter          E    =           
0022809
 Z    =        1274831
29                 I    =           51
80920
 XDOT =       -363
761441                 Wp   =           47
78231
 YDOT =      -4972
774925  meter/sec      RA   =          153
80745  deg
 ZDOT =       5876
356960                 TA   =          326
17661
                                          MA   =          326
32189
                                          Ha   =            195
889  n
mi
                                          Hp   =            184
321

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20662921
37                 X    =        -6325928
24
 Y    =        6497334
04  feet           Y    =         1909802
79  meter
 Z    =        4182517
35                 Z    =         1244168
16
 XDOT =      -1193
443048                 XDOT =        -336
673926
 YDOT =     -16314
878363  feet/sec       YDOT =       -4976
691954  meter/sec
 ZDOT =      19279
386353                 ZDOT =        5874
655039

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8822468
59                 X    =        -2689088
43
 Y    =      -19807696
30  feet           Y    =        -6037385
83  meter
 Z    =        4060090
59                 Z    =         1237515
61
 XDOT =      14613
013138                 XDOT =        4454
046404
 YDOT =      -2522
646645  feet/sec       YDOT =        -768
902697  meter/sec
 ZDOT =      19272
526630                 ZDOT =        5874
266117


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10183
05403303  
00016717  00000-0  10270-3 0  9143
2 25544  51
6440 154
4974 0009554  31
2159 328
9569 15
72143195 25816


Satellite: ISS
Catalog Number: 25544
Epoch time:      10183
05403303   =   yrday
fracday
Element set:     914
Inclination:       51
6440  deg
RA of node:       154
4974  deg
Eccentricity:     
0009554     
Arg of perigee:    31
2159  deg
Mean anomaly:     328
9569  deg
Mean motion:   15
72143195  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2581
Checksum:              303

INTERNATIONAL SPACE STATION ORBITAL DATA:

The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:

NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission

By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command

   David Cottle
   Director Of Engineering
   IDB Communications

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